ES2166234A1 - Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales. - Google Patents

Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales.

Info

Publication number
ES2166234A1
ES2166234A1 ES009802421A ES9802421A ES2166234A1 ES 2166234 A1 ES2166234 A1 ES 2166234A1 ES 009802421 A ES009802421 A ES 009802421A ES 9802421 A ES9802421 A ES 9802421A ES 2166234 A1 ES2166234 A1 ES 2166234A1
Authority
ES
Spain
Prior art keywords
coupled
structures
components
rigidity
modification
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
ES009802421A
Other languages
English (en)
Other versions
ES2166234B1 (es
Inventor
Doncel Miguel Lancho
Revuelta Enrique Cabrera
Castan Fernando Cespedosa
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space SA
Original Assignee
Construcciones Aeronauticas CASA SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Construcciones Aeronauticas CASA SA filed Critical Construcciones Aeronauticas CASA SA
Priority to ES009802421A priority Critical patent/ES2166234B1/es
Priority to US09/334,141 priority patent/US6305871B1/en
Priority to CN99109839A priority patent/CN1107615C/zh
Priority to JP11227724A priority patent/JP2000154667A/ja
Priority to AT99500146T priority patent/ATE252017T1/de
Priority to EP99500146A priority patent/EP1002717B1/en
Priority to DE69912070T priority patent/DE69912070T2/de
Priority to RU99118173/11A priority patent/RU2237601C2/ru
Priority to CA002287066A priority patent/CA2287066A1/en
Priority to UA99116265A priority patent/UA61950C2/uk
Publication of ES2166234A1 publication Critical patent/ES2166234A1/es
Application granted granted Critical
Publication of ES2166234B1 publication Critical patent/ES2166234B1/es
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F3/00—Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors
    • B64G1/6425—Interstage or payload connectors arrangements for damping vibrations
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00—Vibration-dampers; Shock-absorbers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/002—Launch systems
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/50—Bridged by diverse connector
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/59—Manually releaseable latch type
    • Y10T403/591—Manually releaseable latch type having operating mechanism
    • Y10T403/593—Remotely actuated
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/21—Elements
    • Y10T74/2121—Flywheel, motion smoothing-type
    • Y10T74/2132—Structural detail, e.g., fiber, held by magnet, etc.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Connection Of Plates (AREA)
  • Road Paving Structures (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Bridges Or Land Bridges (AREA)
  • Body Structure For Vehicles (AREA)
  • Rod-Shaped Construction Members (AREA)

Abstract

Un sistema de modificación de las propiedades de rigidez/amortiguación de uniones estructurales. Comprende al menos una estructura intermedia (3), para recibir, a uno y otro lado, sendas estructuras (1, 2) a acoplar, medios de bloqueo liberables (6), para inmovilizar, en condición acoplada, dichas dos estructuras a acoplar y dicha estructura intermedia; un primero y un segundo conjuntos de elementos biestables (7, 8), siendo las características de resistencia estructural de los elementos del primero diferentes de las de los del, segundo conjunto; estando los elementos del primer conjunto conectados interiormente a una de dichas estructuras a acoplar y a dicha estructura intermedia; estando los elementos del segundo conjunto conectados interiormente a una y otra de dichas estructuras a acoplar; encontrándose dichos elementos biestables en condición inestable cuando todas las citadas estructuras están acopladas juntas. La invención es aplicable al campo de los vehículos espaciales.
ES009802421A 1998-11-18 1998-11-18 Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales. Expired - Fee Related ES2166234B1 (es)

Priority Applications (10)

Application Number Priority Date Filing Date Title
ES009802421A ES2166234B1 (es) 1998-11-18 1998-11-18 Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales.
US09/334,141 US6305871B1 (en) 1998-11-18 1999-06-15 System for the modification of the rigidity and damping properties of structural joints
CN99109839A CN1107615C (zh) 1998-11-18 1999-07-16 一种用于改变结构连接件刚性/阻尼特性的***
JP11227724A JP2000154667A (ja) 1998-11-18 1999-08-11 構造継手の剛性／減衰特性を改変するためのシステム
EP99500146A EP1002717B1 (en) 1998-11-18 1999-08-17 A system for the modification of the rigidity/damping properties of structural joints
DE69912070T DE69912070T2 (de) 1998-11-18 1999-08-17 Ein System zur Änderung der Steifheits/Dämpfungseigenschaften von Strukturverbindungen
AT99500146T ATE252017T1 (de) 1998-11-18 1999-08-17 Ein system zur änderung der steifheits/dämpfungseigenschaften von strukturverbindungen
RU99118173/11A RU2237601C2 (ru) 1998-11-18 1999-08-19 Система для изменения жесткости/демпфирующих свойств силовых соединений
CA002287066A CA2287066A1 (en) 1998-11-18 1999-10-21 A system for the modification of the rigidity/damping properties of structural joints
UA99116265A UA61950C2 (en) 1998-11-18 1999-11-17 System for modification of rigidity/damping properties of structural joints

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES009802421A ES2166234B1 (es) 1998-11-18 1998-11-18 Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales.

Publications (2)

Publication Number Publication Date
ES2166234A1 true ES2166234A1 (es) 2002-04-01
ES2166234B1 ES2166234B1 (es) 2003-02-16

Family

ID=8305834

Family Applications (1)

Application Number Title Priority Date Filing Date
ES009802421A Expired - Fee Related ES2166234B1 (es) 1998-11-18 1998-11-18 Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales.

Country Status (10)

Country Link
US (1) US6305871B1 (es)
EP (1) EP1002717B1 (es)
JP (1) JP2000154667A (es)
CN (1) CN1107615C (es)
AT (1) ATE252017T1 (es)
CA (1) CA2287066A1 (es)
DE (1) DE69912070T2 (es)
ES (1) ES2166234B1 (es)
RU (1) RU2237601C2 (es)
UA (1) UA61950C2 (es)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE515850C2 (sv) * 2000-09-18 2001-10-15 Saab Ericsson Space Ab Anordning och metod vid en rymdfarkost
GB2372976B (en) * 2000-09-18 2004-07-07 Saab Ericsson Space Ab An Adaptor for a Spacecraft
JP4339796B2 (ja) * 2002-12-04 2009-10-07 エーアーデーエセ カサ エスパシオ，ソシエダ リミタダ 減衰装置
US7222823B2 (en) * 2004-07-06 2007-05-29 Ata Engineering, Inc. Payload adapter
US20060145016A1 (en) * 2004-12-30 2006-07-06 The Boeing Company Mating of spacecraft components using shape memory materials
US7748663B1 (en) * 2005-05-24 2010-07-06 Lockheed Martin Corporation Launch vehicle stage integration device
US7866607B2 (en) * 2006-12-21 2011-01-11 Intelsat Piggyback satellite payload arrangement, a device for and method of attaching a piggyback satellite payload and adapter to be used for a piggyback satellite payload arrangement for launching the piggyback satellite
US7905453B2 (en) * 2006-12-21 2011-03-15 Intelsat Piggyback equipment panel payload arrangement, a device for and method of attaching a hosted secondary piggyback payload and adapter to be used for a piggyback secondary payload arrangement for launching the piggyback equipment panel secondary
WO2014176423A1 (en) * 2013-04-24 2014-10-30 Marquette University Variable stiffness actuator with large range of stiffness
US10190537B2 (en) 2013-07-02 2019-01-29 Mra Systems, Inc. Engine and band clamp
CN104058103A (zh) * 2014-06-27 2014-09-24 北京空间飞行器总体设计部 一种用于航天器柔性充气展开结构的刚柔连接结构
CN106864775A (zh) * 2015-12-11 2017-06-20 天津航天瑞莱科技有限公司 一种航天器有效载荷减冲击装置
CA3020920C (en) 2016-04-14 2023-10-31 Marquette University Variable stiffness series elastic actuator
CN108638593A (zh) * 2018-03-09 2018-10-12 北京宇航***工程研究所 一种蜂窝阻尼颗粒冲击减缓装置
CN109693810B (zh) * 2018-12-29 2022-04-26 西北工业大学 一种用于空间碎片清理的纳星结构
CN109823576B (zh) * 2019-02-20 2020-11-24 上海卫星工程研究所 用于行星着陆器的承载连接结构
CN111619831B (zh) * 2020-04-29 2021-11-16 航天东方红卫星有限公司 一种连杆式星箭分离机构
CN112249364A (zh) * 2020-10-28 2021-01-22 哈尔滨工业大学 小卫星的结构***、小卫星及组装小卫星的方法
CN113152708A (zh) * 2021-02-10 2021-07-23 国机集团科学技术研究院有限公司 以水平抗震为主的振震双控控制策略
CN113415440B (zh) * 2021-07-20 2022-06-17 哈尔滨工业大学 一种快速展开支撑装置

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3529417A (en) * 1967-11-16 1970-09-22 Trw Inc Fluid pressure actuated linear force generating means
JPH03148400A (ja) * 1989-11-02 1991-06-25 Natl Space Dev Agency Japan<Nasda> 衛星とロケットおよびアポジ・キック・エンジンとの結合／分離方法
US5244170A (en) * 1991-10-15 1993-09-14 General Dynamics Corporation, Space Systems Division Passive nonlinear interface strut (PNIS)
US5352061A (en) * 1993-01-05 1994-10-04 Honeywell Inc. Anti-rotation ring joint

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3346929A (en) * 1966-03-04 1967-10-17 James E Webb Latching mechanism
US3458217A (en) * 1966-11-25 1969-07-29 Joseph D Pride Jr Tubular coupling having low profile band segments with means for preventing relative rotation
US3505925A (en) * 1967-10-16 1970-04-14 Mc Donnell Douglas Corp Structure release system
US3633456A (en) * 1969-07-03 1972-01-11 Mc Donnell Douglas Corp Power-actuated separation system
US3564564A (en) * 1969-11-21 1971-02-16 Nasa Latching mechanism
US3737117A (en) * 1971-07-06 1973-06-05 Nasa Docking structure for spacecraft
FR2516893A1 (fr) * 1981-11-26 1983-05-27 Aerospatiale Systeme permettant le maintien temporaire et la liberation de deux parties, plus particulierement dans le domaine spatial
FR2648199B1 (fr) 1989-06-09 1991-09-27 Aerospatiale Dispositif de liaison temporaire, notamment pour appendice de satellite artificiel, et procede de liberation d'une telle liaison
FR2664338B1 (fr) 1990-07-04 1992-10-23 Aerospatiale Dispositif de liaison entre deux objets par plusieurs points de fixation.
FR2735099B1 (fr) * 1995-06-06 1997-08-29 Aerospatiale Dispositif adaptateur basculant pour l'emport de plusieurs charges utiles sur un meme lanceur.
ES2120338B1 (es) 1995-10-16 1999-05-01 Const Aeronauticas Sa Sistema de fijacion y separacion para satelites.
US5961078A (en) * 1997-06-27 1999-10-05 Mcdonnell Douglas Corporation Passive axial vibration isolation system for a spacecraft launch vehicle
ES2131476B1 (es) 1997-09-26 2000-03-01 Const Aeronauticas Sa Sistema de fijacion y separacion de satelites.

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3529417A (en) * 1967-11-16 1970-09-22 Trw Inc Fluid pressure actuated linear force generating means
JPH03148400A (ja) * 1989-11-02 1991-06-25 Natl Space Dev Agency Japan<Nasda> 衛星とロケットおよびアポジ・キック・エンジンとの結合／分離方法
US5244170A (en) * 1991-10-15 1993-09-14 General Dynamics Corporation, Space Systems Division Passive nonlinear interface strut (PNIS)
US5352061A (en) * 1993-01-05 1994-10-04 Honeywell Inc. Anti-rotation ring joint

Also Published As

Publication number Publication date
EP1002717B1 (en) 2003-10-15
CA2287066A1 (en) 2000-05-18
CN1107615C (zh) 2003-05-07
EP1002717A3 (en) 2000-10-11
DE69912070D1 (de) 2003-11-20
EP1002717A2 (en) 2000-05-24
DE69912070T2 (de) 2004-08-05
CN1253898A (zh) 2000-05-24
RU2237601C2 (ru) 2004-10-10
UA61950C2 (en) 2003-12-15
ATE252017T1 (de) 2003-11-15
JP2000154667A (ja) 2000-06-06
ES2166234B1 (es) 2003-02-16
US6305871B1 (en) 2001-10-23

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